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DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE LAMINATES USING SURROGATE MODELS FOR MINIMUM COMPLIANCE OF CURVED WING PANELS
Date
2021-09-10
Author
İNCİ, HASAN
Kayran, Altan
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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URI
http://aiac.ae.metu.edu.tr/paper.php?No=AIAC-2021-064
https://hdl.handle.net/11511/99995
Conference Name
11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE
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Department of Aerospace Engineering, Conference / Seminar
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BibTeX
H. İNCİ and A. Kayran, “DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE LAMINATES USING SURROGATE MODELS FOR MINIMUM COMPLIANCE OF CURVED WING PANELS,” presented at the 11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 2021, Accessed: 00, 2022. [Online]. Available: http://aiac.ae.metu.edu.tr/paper.php?No=AIAC-2021-064.
